N250PS, cancelled Dec 9, 2025

Service difficulty reports · 89

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N250PS' AND deregistration_id = 'N250PS-2025-12-09'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR VNAA2020031921101Flashlight · inoperativeFWD FA FLASHLIGHT INOP. MX REMOVED AND REPLACED FWD FA FLASHLIGHT. OPS CHECK GOOD.Mar 16, 2020 · N250PS · Cndair CL6002B19 · Emergency EquipmentSDR VNAA2020031101101Tube · crackedUNCOMMANDED DECELERATION OF RH ENGINE IN FLIGHT APROX 8% N1. MAINTENANCE FOUND THE T2 ANTI ICE TUBE ASSY CRACKED, REMOVED AND AND REPLACED THE TUBE ASSY OPS CHECK GOOD.Mar 8, 2020 · N250PS · Cndair CL6002B19 · Engine Anti-Icing SystemSDR VNAA2020030511101Bpsu · out of rigON FINAL APPROACH INTO LGA, THE CREW PULLED FLAPS FROM 8-20, BUT FLAPS DID NOT MOVE, AND A FLAP FAILURE MESSAGE APPEARED. THE CREW EXECUTED A GO AROUND, AND DECIDED TO DIVERT TO JFK TO LAND ON A LONGER RUNWAY. THE CREW DID DECLARE AN EMERGENCY. THE AIRCRAFT LAMar 2, 2020 · N250PS · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR VNAA2020021261102Engine · oscillatesAT 27000 FEET RIGHT ENGINE N1 OSCILLATED BETWEEN 81 TO 88 SLOWED THE PLANE AND IT STEADIED OUT. CONTINUED THE FLIGHT. PERFORMED ENG. RUN & CHECK N1 SPEED-CONTROL AMP. CHK. FOUND OK AND NO N1 OSCILLATION AT THIS TIME.Jan 26, 2020 · N250PS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR VNAA2019123091101Wire · disconnectedEXIT SIGN EMERGENCY LIGHT BY PAX DOOR INOP. FOUND WIRE UNPLUGGED. CONNECTED THE WIRE IAW AMM 33-51-10-400-801. OPS CHECK GOOD.Dec 29, 2019 · N250PS · Cndair CL6002B19 · Light System WiringSDR VNAA2019121011101Sensor · dirtyAT 800 FT AFTER TAKEOFF, THE CREW OBSERVED AND FELT THE RH N1 SURGE. CREW LEVELED OFF AT 5000 FT, RAN QRH, AND RETURNED TO THE FIELD. THE CREW DID NOT DECLARE AN EMERGENCY BUT ATC DID ROLL THE FIRETRUCKS. DEFERRED RH ENG SPEED CONTROL SYSTEM. MX CLEANED T2 SEDec 10, 2019 · N250PS · Cndair CL6002B19 · Engine ControlsSDR VNAA2019082097111Pump · failedON CLIMB OUT AT FL100 ENGINE 1 OIL TEMP READ OUT FLASHED RED INDICATING HIGH OIL TEMP. CREW REQUESTED LEVEL OFF WITH ATC, BACKED ENGINE POWER DOWN AND RAN THE QRH. QRH INSTRUCTED TO SHUT DOWN ENGINE AND LAND AT NEAREST SUITABLE. CREW DECLARED AN EMERGENCY WAug 17, 2019 · N250PS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR VNAA2019073011101Power Supply · failedCENTER AISLE EMERGENCY EXIT/FWD SIGN LIGHT INOP. R&R EMERGENCY BATTERY SUPPLY. IAW CRJ200 AMM 33-51-04-000/400-801. OPS CHECK GOOD.Jul 30, 2019 · N250PS · Cndair CL6002B19 · Emergency LightingSDR VNAA2019020199913Floorbeam · crackedR/H FS484.00 ANGLES @ RBL27 & RBL36 ARE CRACKED. C/A: REMOVED AND REPLACED ANGLE IAW CRJ 200 SRM 51-40-11, & 51-42-21Feb 1, 2019 · N250PS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR VNAA2019020199912Floorbeam · crackedL/H FS484.00 ANGLES @ LBL27 & LBL36 ARE CRACKED. C/A: REMOVED AND REPLACED ANGLE IAW CRJ 200 SRM 51-40-11, & 51-42-21Feb 1, 2019 · N250PS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR VNAA2019020199911Floor Support · corrodedFLOOR SUPPORT ANGLES AND CUPS AT PAX DOOR SILL ARE CORRODED FROM F.S. 310 TO F.S. 349. C/A: REMOVED AND REPLACED PAX DOOR FLOOR SUPPORT ANGLES AND CUPS REF CRJ 200 SRM 51-42-06, 51-42-13 & 51-42-21.Feb 1, 2019 · N250PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2019020199910Seat Track · corrodedLBL9 AND RBL9 FS364-399 FLOOR SEAT TRACK SEGMENTS HAVE CORROSION. C/A: REMOVED AND REPLACED TRACK SEGMENT IAW BOMBARDIER REO 601R-53-00-485.Feb 1, 2019 · N250PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2019020199909Seat Track · crackedLBL9 AND RBL9 FS399-409+120 FLOOR SEAT TRACK SEGMENTS HAVE CORROSION. C/A: REMOVED AND REPLACED TRACK SEGMENT IAW BOMBARDIER REO 601R-53-00-485.Feb 1, 2019 · N250PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2019020199908Stiffener · crackedPAX DOOR ASSIST MOTOR CRACKED AT WEB SIDE ATTACH POINT. C/A: REMOVED AND REPLACED PAX DOOR SIDE PANEL STIFFENER REF CRJ 200 SRM 51-42-15.Feb 1, 2019 · N250PS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR VNAA2019020199907Frame · crackedFS 333.0 FRAME IS CRACKED BETWEEN STRINGER 0 AND STRINGER 1L. C/A: REMOVED AND REPLACED FRAME IAW CRJ 200SRM 51-40-11,51-42-21 AND 51-42-06.Feb 1, 2019 · N250PS · Cndair CL6002B19 · Fuselage Main, FrameSDR VNAA2019020199906Trunnion · crackedL/H LOWER WING PLANK MLG TRUNNION FASTENER HOLE (FWD LOOKING AFT) HAS AN INDICATION AT 5TH FASTENER HOLE FROM THE FWD EDGE OF STEEL STRAP AT 55% FSH, FAILED NDT. C/A: REPAIRED L/H LOWER WING PLANK MLG TRUNNION FASTENER HOLE IAW BOMBARDIER REO 601R-57-21-2938 RFeb 1, 2019 · N250PS · Cndair CL6002B19 · Wing, Landing Gear Attach FittingsSDR VNAA2019020199905Trunnion · crackedL/H LOWER WING PLANK MLG TRUNNIION FASTENER HOLE (FWD LOOKING AFT) HAS AN INDICATION AT 2ND FASTENER HOLE FROM THE FWD EDGE OF STEEL STRAP AT 60% FSH FAILED NDT. C/A: REPAIRED L/H LOWER WING PLANK MLG TRUNNION FASTENER HOLE IAW BOMBARDIER REO 601R-57-21-2938 RFeb 1, 2019 · N250PS · Cndair CL6002B19 · Wing, Landing Gear Attach FittingsSDR VNAA2019020199904Trunnion · crackedFOUND INDICATION ON R/H TRUNNION 7TH HOLE FROM AFT TO STRAP 90% FSH APPROX. 0.5 UP THE TRUNNION FAILS NDT. C/A: REPAIRED R/H TRUNNION DAMAGED FASTENER HOLE IAW BOMBARDIER REO 601R-57-21-2939 REV.--DATED 2019-01-24.Feb 1, 2019 · N250PS · Cndair CL6002B19 · Wing, Landing Gear Attach FittingsSDR VNAA2019020199903Trunnion · crackedFOUND INDICATION ON R/H TRUNNION 4TH HOLE FROM AFT OF STRAP 60% FSH APPROX. 0.75 UP THE TRUNNION FAILS NDT. C/A: REPAIRED R/H TRUNNION DAMAGED FASTENER HOLE IAW BOMBARDIER REO 601R-57-21-2939 REV.--DATED 2019-01-24.Feb 1, 2019 · N250PS · Cndair CL6002B19 · Wing, Landing Gear Attach FittingsSDR VNAA2019020199902Angle · crackedFS409+128 BLO RH VERTICAL POST ANGLE HAS AN INDICATION .15" LONG BY 80% FSH IN THE UPPER AFT RADIUS WL69. C/A: REMOVED AND REPLACED ANGLE IAW CRJ 200 SRM 51-40-11,51-42-22 AND 51-42-06.Feb 1, 2019 · N250PS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR VNAA2019020199901Seal Depressor · corrodedPAX DOOR LOWER SEAL SURROUND CORRODED. C/A: REMOVED AND REPLACED PAX DOOR LOWER SEAL SURROUND IAW CRJ 200 SRM 51-40-11 AND 51-42-06.Feb 1, 2019 · N250PS · Cndair CL6002B19 · Fuselage Main, StructureSDR VNAA2018091711101Loop · contaminatedCREW RECEIVED A L 10TH DUCT RED MSG. RAN THE QRH AND CAUTION DID NOT CLEAR. DECLARED AN EMERGENCY AND LANDED IN GSO. CLT MX GOING TO GSO WITH PARTS. CLT MX FOUND LOOPS SUBMERGED IN WATER IN AFT EQUIP BAY, CLEANED OUT WATER/LOOPS, CHECK GOOD.Sep 10, 2018 · N250PS · Cndair CL6002B19 · Pneumatic Indicating SystemSDR VNAA2018021611102Warning Message · activatedTHE CREW RECEIVED AN ANTI-ICE DUCT SYSTEM MESSAGE. THE CREW RAN THE QRH AND DECLARED AN EMERGENCY TO CLIMB OUT OF ICING CONDITIONS. THE CREW CONTINUED TO THEIR DESTINATION AND LANDED WITHOUT INCIDENT. OPEN.Feb 16, 2018 · N250PS · Cndair CL6002B19 · Ice/Rain Protection SystemSDR VNAA2017082911102Controller · malfunctionedAFTER DEPARTURE, THE CREW RECEIVED A LEFT WINDSHIELD HEAT CAUTION MESSAGE AND NOTICED A SLIGHT ODOR. THE QUICK REFERENCE HANDBOOK WAS FOLLOWED AND CYCLED SYSTEM. AFTER CYCLING THE SYSTEM THE CREW OBSERVED SMOKE AND TURNED THE WINDSHIELD HEAT OFF. THE AIRCRAFT Aug 29, 2017 · N250PS · Cndair CL6002B19 · Windshield/Door Rain/Ice RemovalSDR VNAA2017082811102Unknown · odorBURNING ODOR FROM LEFT PACK ON GROUND. PERFORMED AN OPS CHECK OF THE LT PACK, OPS CHECKED GOOD.Aug 28, 2017 · N250PS · Cndair CL6002B19 · Cabin Cooling SystemSDR VNAA2017012300030Skin · damagedEXTERNAL FUSELAGE SKIN AT BS 235 BETWEEN STRINGERS 26L AND 26R DAMAGED. PERFORMED A MAJOR REPAIR.Jan 23, 2017 · N250PS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR VNAA2016071800018Control Unit · malfunctionedLEFT JET OVERHEAT FAIL MESSAGE IN FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R FIRE AND OVERHEAT CONTROL UNIT AND PERFORMED CHECKS IAW AMM.Jul 18, 2016 · N250PS · Cndair CL6002B19 · Overheat DetectionSDR VNAA2016071800017Overheat Sensor · out of positionLEFT JET OVERHEAT FAIL MESSAGE IN FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED JETPIPE SENSING ELEMENTS AND FOUND LOOP-A SENSING ELEMENT TOUCHING A CLAMP. MAINTENANCE REPOSITIONED LOOP AND PERFORMED CHECKS IAW AMM.Jul 18, 2016 · N250PS · Cndair CL6002B19 · Overheat DetectionSDR VNAA2016070400005Air Filter · faultyLEFT HIGH PRESSURE CAUTION MESSAGE AT 8000 FEET. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE LT 10TH STAGE PRESSURE SHUTOFF VALVE INLET FILTER AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICJul 4, 2016 · N250PS · Cndair CL6002B19 · Air Distribution SystemSDR VNAA2016062300025Strip · missingROW EMERGENCY LIGHTS COLOR STRIPPING MISSING. MAINTENANCE INSPECTED, REINSTALLED PHOTOLUMINESCENT FLOOR MARKING AND COVER, AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.Jun 23, 2016 · N250PS · Cndair CL6002B19 · Emergency LightingSDR VNAA2015091000014Windshield · delaminatedCREW REPORTED SEVERE DELAMINATION ON LT FORWARD WINDSHIELD AND WINDSHIELD ARCING. MAINTENANCE INSPECTED, R & R CAPTAIN’S WINDSHIELD AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Sep 10, 2015 · N250PS · Cndair CL6002B19 · Flight Compartment WindowsSDR VNAA2015091000015Controller · failedCREW REPORTED SEVERE DELAMINATION ON LT FORWARD WINDSHIELD AND WINDSHIELD ARCING. MAINTENANCE INSPECTED, R & R CAPTAIN’S WINDSHIELD TEMPERATURE CONTROLLER AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Sep 10, 2015 · N250PS · Cndair CL6002B19 · Windshield/Door Rain/Ice RemovalSDR VNAA2015062800041Hose · leakingON APPROACH, CREW REPORTED HYD SYS NR 3 LOW PRESSURE MESSAGE CAME ON WHEN LANDING GEAR SELECTED DOWN. CREW LANDED AND USING DIFFERENTIAL BRAKING, TAXIED TO GATE. MAINTENANCE TROUBLESHOT AND FOUND LEAK ON AFT SIDE OF ALTERNATING CURRENT MOTOR PUMP, ACMP, 3B. Jun 28, 2015 · N250PS · Cndair CL6002B19 · Hydraulic System, MainSDR VNAA2015062800040Hose · leakingON APPROACH, CREW REPORTED HYDRAULIC SYSTEM NR 3 LOW PRESSURE MESSAGE CAME ON WHEN LANDING GEAR SELECTED DOWN. CREW LANDED AND USING DIFFERENTIAL BRAKING, TAXIED TO GATE. MAINTENANCE TROUBLESHOT AND FOUND LEAK ON AFT SIDE OF ALTERNATING CURRENT MOTOR PUMP, AJun 28, 2015 · N250PS · Cndair CL6002B19 · Hydraulic System, MainSDR VNAA2015032600026Structure · corrodedIN PASSENGER COMPARTMENT AT PASSENGER DOOR CUTOUT ON FS 310.00 AND FS 349.00, THE PASSENGER DOOR COUNTER BALANCE ANCHOR FITTING SERATED PLATES HAVE EXFOLIATION CORROSION. REMOVED CORRODED PLATES AND INSTALLED NEW SERVICABLE PLATES IAW AMM 52-11-17-400-804.Mar 26, 2015 · N250PS · Cndair CL6002B19 · Fuselage Main, StructureSDR VNAA2014071200006Sensor · malfunctionedCREW REPORTED LT 14TH DUCT RED WARNING MESSAGE WHILE DESCENDING THROUGH 14,000 FT. CREW COMPLIED WITH QRH. MESSAGE DID NOT EXTINGUISH IMMEDIATELY, BUT DID EXTINGUISH SHORTLY BEFORE LANDING. DECLARED AN EMERGENCY AND LANDED SAFELY. MAINTENANCE TROUBLESHOT, Jul 12, 2014 · N250PS · Cndair CL6002B19 · Pneumatic Distribution SystemSDR VNAA2013062800018Downlock Sensor · faultyCREW REPORTED TRIPLE CHIME AND GEAR DISAGREE AMBER NOSEWHEEL INDICATION ON DESCENT. CREW PERFORMED MANUAL GEAR EXTENSION AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED NOSE LANDING GEAR NUMBER TWO (2) DOWNLOCK SENSOR AND PERFORMED GJun 28, 2013 · N250PS · Cndair CL6002B19 · Landing Gear Position and WarningSDR VNAA2013052700016Bulkhead · crackedDURING SCHEDULED MAINTENANCE FS 621 PRESSURE BULKHEAD HAD INDICATION OF CRACK. THE AREA WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.May 27, 2013 · N250PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2013052700015Structure · damagedDURING SCHEDULED MAINTENANCE FS 589.0 TO FS 605.0 DAMGE WAS FOUND. THE AREA WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.May 27, 2013 · N250PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2013042400017Light · inoperativeEMERGENCY FLOOR LIGHTING AT SEATS 4F/D REPORTED INOPERATIVE. MAINTENANCE INSPECTED, REMOVED AND REPLACED EMERGENCY FLOOR TRACK LIGHTING AT SEAT 4F/D AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.Apr 24, 2013 · N250PS · Cndair CL6002B19 · Emergency LightingSDR VNAA2013042300016Battery Pack · dischargedCREW REPORTED EMERGENCY LIGHTS ON THE FLOOR BETWEEN ROWS TWO (2) TO FIVE (5) INTERMITTENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED NUMBER TWO (2) EMERGENCY LIGHT BATTERY PACK AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOApr 23, 2013 · N250PS · Cndair CL6002B19 · Emergency LightingSDR VNAA2013031800013Seal · leakingCREW REPORTED RIGHT 14TH DUCT RED MESSAGE DURING FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND RIGHT ENGINE 14TH STAGE DUCT COUPLING FROM ENGINE TO PYLON TO BE LEAKING. MAINTENANCE REMOVED AND REPLACED E-SEALS AMar 18, 2013 · N250PS · Cndair CL6002B19 · Air Intake Anti/De-Ice SystemSDR VNAA2013022700017Engine · failedCREW REPORTED A HIGH ITT AND VIBRATION WITH LOSS OF POWER IN NR 2 ENGINE. CREW RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED, REPLACED, AND OPERATIONAL CHECKED THE NR 2 ENGINE USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFTFeb 27, 2013 · N250PS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR VNAA2012091600018Bulkhead · crackedDURING SCHEDULED MAINTENANCE FOUND FS 202.75 PRESSURE BULKHEAD WEB CRACKED. FS 202.75 PRESSURE BULKHEAD WEB WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.Sep 23, 2012 · N250PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2012082100016Windshield · crackedCREW REPORTED THE RIGHT WINDSHIELD CRACKED. AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED, AND REPLACED THE RIGHT WINDSHIELD USING AIRCRAFT MAINTENANCE MANUALS. OPERATIONAL CHECKS WERE ACCOMPLISHED USING THE AIRCRAFT MAINTEAug 21, 2012 · N250PS · Cndair CL6002B19 · Flight Compartment WindowsSDR VNAA2011091500013Fairing · damagedAT PHL, CREW REPORTED RIGHT WING AFT INBOARD FLAP FAIRING HAD BURN MARK / FRAYING AREA. MAINTENANCE INSPECTED AIRCRAFT AND REPAIRED LIGHTNING STRIKE DAMAGE TO RIGHT WING AFT INBOARD FLAP FAIRING. MAINTENANCE REPAIRED DAMAGED PAINT ON LEFT LOWER AFT WINGLET ASep 11, 2011 · N250PS · Cndair CL6002B19 · Trailing Edge FlapsSDR VNAA2011082500013Connector · looseCREW REPORTED RANDOM GEAR HORN IN FLIGHT. RED GEAR DISAGREE MESSAGE AND RED NOSE DOOR OPEN MESSAGE REPORTED AFTER SELECTING GEAR DOWN ON APPROACH TO MOB. AIRCRAFT LANDED IN MOB WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, TIGHTENED PROXIMITY SENSOR CABLE CONNAug 20, 2011 · N250PS · Cndair CL6002B19 · Door System WiringSDR VNAA2011081000006Post · crackedDURING SCHEDULED MAINTENANCE THE VERTICLE POST FS718.0 WAS FOUND CRACKED. THE AIRCRAFT WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.Aug 7, 2011 · N250PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2011081000005Post · crackedDURING SCHEDULED MAINTENANCE THE VERTICLE POST FS 409+128 WAS FOUND CRACKED. THE AIRCRAFT WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.Aug 7, 2011 · N250PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2011081000004Angle · corrodedDURING SCHEDULED MAINTENANCE THE FLOORBEAM CAP ANGLE BETWEEN FS 574 AND FS 608 AT LBL 27 WAS FOUND CORRODED. THE AIRCRAFT WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.Aug 7, 2011 · N250PS · Cndair CL6002B19 · Fuselage Main, Floor Beam
Back to N250PS, cancelled Dec 9, 2025